Flexible barrier member useful in aerosol dispensers

Abstract: A barrier for use in a pressurized container (22) comprising a unitary flexible and expandable member (11) having an outer wall segment (12) terminating in a sealing flange (16) and an inner wall segment (14) joined to the outer wall segment (12) through a fold (15) and a central piston region (20) emerging from the terminus of the inner wall segment (14) distal to the fold (15); the barrier (10) being sufficiently thick and rigid to be freestanding before incorporation into a pressurized container (22). The outer and (12) inner wall (14) segments are oppositely-directed frustoconial shapes forming a small acute angle with each other. The outer (12) and inner (14) wall segments expand outwardly to progressively conform to the container inner wall surface (23) as product is evacuated from the container (22). The outer wall segment (12) may be thicker and more rigid than the inner wall segment (14). The barrier is nestable with like barriers.

Description: Background of the Invention 1. Field of the Invention This invention relates to pressurized dispenser packages, such as aerosol packages, wherein the product to be dispensed and the pressure-generating media, i.e. the propellant, are maintained in isolation through separation on opposite sides of a barrier. An aerosol package of this type is generally referred to as a "barrier pack" aerosol package. 2. Description of the Prior Art Aerosol barrier packs of the prior art have been of at least three general types. In the piston-type barrier pack the barrier is a piston-like component that is mounted in the container in sliding relation to the inside surface of the container. The product to be dispensed is disposed on the valved side of the piston and the propellant, which generates pressure within the container, is on the opposite side of the piston. In Aerosol Handbook, Second Edition, 1982, there is described a piston-type aerosol dispenser marketed by American Can Company under the trade-name "Mira-Flo". In the Mira-Flo dispenser the piston skirt is designed to seal against the sides of the container to prevent the propellant gas from passing into the product chamber on the other side of the piston. Actuation of the aerosol discharge valve causes a reduction in pressure in the product chamber thereby resulting in the pressure in the propellant chamber urging the piston toward the discharge valve and causing the discharge of product through the discharge valve. Examples of a piston-type barrier pack are described in United States Patent Nos. 3,022,923, 3,756,476 and 3,929,132. In a second type of aerosol barrier pack, a flexible, collapsible bag is affixed within the container opening either to the aerosol discharge valve or to the bead of the container opening. The Continental Can Company in the late 1960's introduced an aerosol barrier dispenser known as the "Sepro-Can". The Sepro-Can includes an interior plastic product bag having an opening that is attached to the valve opening at the top of the container. The side walls of the bag extend along the side walls of the container and are pleated like an accordion so the bag can collapse inward and upward under the influence of pressure in the remainder of the container as the bag is emptied. Patents which illustrate a barrier pack of the second type are set forth in U.S. Patent Nos. 3,788,521, 3,896,970 and 4,067,499. Modifications of barrier packs of the second type include attaching the bag to the side wall of the container or to the joint formed between the side wall of the container and the top of the container. A third type of prior art barrier pack is an unfolding cup-shaped barrier wherein the barrier has an outer wall terminating in a sealing flange, said outer wall being disposed contiguous to the inner wall of the container. The inner wall of the barrier is initially folded within the outer wall, the inner wall terminating in an end closing portion. The barrier is contained in a valved aerosol container and sealed at the joint formed between the sidewall and the bottom end closure of the container. Product is admitted through the valved opening of the container and propellant through a port in the bottom end closure of the container. Actuation of the valve reduces the pressure in the product compartment and results in the inner wall of the barrier unfolding from within the outer wall of the barrier and causing the end-closing portion of the inner wall of the barrier to advance and thereby urge the product toward the discharge valve. A patent which illustrates the third type of prior art barrier pack is U.S. Patent No. 3,109,463. A problem with the piston-type barrier pack of the first type is the imperfect seal between the side skirt of the piston and the side wall of the container which allows propellant to seep into the product with consequent discharge of propellant during product discharge as well as contamination of the product with propellant. Also, it is not uncommon for aerosol containers to be dented and thus lose their true circumferential shape, with the consequence that the piston is incapable of axial movement within the container past the aberrant configuration. A problem with barrier packs of the second type wherein the barrier is affixed to the valve or valve opening of the container is that the barrier collapses in a manner to cause pocketing of the product within the collapsible barrier with consequent undesirable diminution of the evacuation of the product from the container. In the third type of prior art barrier pack described herein, the unfolding cup-shape barrier does not advance progressively and uniformly against the inner wall of the container but tends to pocket and entrap product against the wall or within pockets formed in the barrier itself as it unfolds. Attempts to solve these problems have included adding an additional rigid piston to the end-closing portion of the inner wall, or adhering the outer wall of the barrier in peelable fashion to the inner wall of the container. Generally, barriers of the third type can be difficult to form, as well as to insert into and seal with the container. Further, in US 3,494,513 there is disclosed a spacecraft propellant tank comprising an internal diaphragm against which pressured gas is applied to expand and displace the diaphragm thereby expelling the propellants from the tank. Moreover, there is known from US 3,415,425 an aerosol dispenser including a unitary flexible barrier for use in a plural-zoned, valved pressure container comprising a shaped spatial form having a terminal sealing means, a flexible and expandable wall portion, and a central piston region, wherein the sealing means, wall portion and piston region are formed as a unitary spatial form with sufficient rigidity to maintain its shape prior to insertion into and use in a plural-zoned pressure container. The terminal sealing means is adapted for sealing in a container to form a propellant zone and a product zone, and the flexible and expandable wall portion has an inner wall segment and an outer wall segment connected by a fold. The outer wall segment and the inner wall segment are substantially of a cylindrical shape, the outer wall segment extending from the terminal sealing means to the fold and the inner wall segment extending from the fold. Further, the central piston region is connected to and extends generally inwardly from the bottom of the inner wall segment to close and complete said unitary barrier member. The inner wall segment has sufficient flexibility to permit said inner wall segment and said central piston region to move in an axially direction under the influence of propellant pressure and the outer wall segment has sufficient expandability to expand outwardly under the influence of propellant pressure to progressively substantially conform to the inner side container surface from the terminal sealing means to the fold, and the inner wall segment has sufficient expandability to expand outwardly under the influence of propellant pressure to substantially conform to the inner side container surface from the fold. SUMMARY OF THE INVENTION In view of this closest prior art known from US 3,415,425, it is an object of the present invention to provide a unitary flexible and expandable barrier for use in a plural-zoned, valved pressure container, which is easy to manufacture and ship, which is easy to insert into and seal to the container, which prevents leakage of the fluids from one compartment to the other compartment, and which does not pocket and therefore precludes evacuation of significant amounts of the product to be discharged. This object is achieved by the unitary flexible and expandable barrier as defined in claim 1. By virtue of having sufficient rigidity to maintain its shape prior to insertion into the container, as well as the presence of the tapered outer wall segment, the barrier of the present invention is very easily insertable into the bottom of the container. Further, the outer wall segment is, at the initial state, thicker and more rigid than the inner wall segment at the initial state. By virtue of the tapered outer and inner wall segments, the barrier is nestable with like barriers for convenience and cost savings in shipping. Further, the nesting facilitates fast and simple machine feeding of stacked barriers sequentially into the containers. In a preferred form of the invention the inner wall segment also is of slightly less length than the outer wall segment; and the sealing means is a radially extending flange which acts as a gasket between the bottom of the sidewall of the container and the bottom closure of the container. The central piston region also may be thicker than the inner wall segment. The overall length of the flexible and expandable wall portions and the contour of the central piston region is designed such that the barrier upon full evacuation of the product from the pressurized container will tend to press against all inner surfaces of the container to thereby maximize the evacuation of the container contents. A particularly advantageous material for barriers is polyethylene terephthalate (PET). Where permeation across the barrier is a concern, the barrier of the present invention may utilize a unitary multi-layer configuration. Such multi-layer configurations, their materials of construction and their manufacture, are well known to those skilled in the art. Generally, in a three-layer system, the inner layer is a material that prevents transport of propellant and product therethrough and the outer layers are inert to the propellant and product. Brief Description of the Drawings Figure 1 is an elevational cross-sectional view of an embodiment of the barrier of this invention. Figure 2 is an elevational cross-sectional view of the barrier of Figure 1 positioned within an empty aerosol container with the top opening of the container shown in schematic and the aerosol valve not shown. Figure 3 is a schematic cross-sectional view of an embodiment for forming the seal between the barrier sealing means, the sidewall of the container and the bottom closure of the container. Figures 4a and 4b are schematic views of the barrier of this invention within an aerosol container showing, in Figure 4a, the barrier in an initial position a short period of time after loading the container with product and propellant; and, in Figure 4(b) the ultimate contour of the barrier after evacuation of the product from the container. Figure 5 is a partial cross-sectional view of a multilayered barrier of the present invention. Figure 6 is a cross-sectional view of an embodiment of the central piston region of the barrier of this invention. Figure 7 shows barriers of this invention in a nesting relation. Figure 8 is a schematic diagram of the several steps used in fabricating the barrier pack of this invention from a plastic sheet. Figure 9 is a schematic of the thermoforming equipment used in forming the barrier pack of this invention. Detailed Description of the Invention Referring now to the drawings, Figure 1 shows a unitary barrier generally designated at 10, as it is initially formed, said barrier having a wall 11 comprising a flexible and expandable outer wall segment 12 and a flexible and expandable inner wall segment 14 connected by a fold 15, the outer wall segment 12 terminating in a sealing flange 16. At the terminus 18 of the inner wall segment 14, central piston region 20 extends inwardly to close the barrier. It should be noted that the outer wall segment 12 has a steeply frusto-conical shape extending from the sealing flange 16 to the fold 15, and that the inner wall segment 14 has a steeply frustoconical shape oppositely directed to the outer wall segment 12 extending from the fold 15 to the central piston region 20. The outer wall segment 12, including the sealing flange 16, is sufficiently thick and rigid to impart a shaped spatial form to the barrier and causes the barrier to be free-standing and ready for insertion into the container. It has been found that a barrier formed of PET with the following dimensions has performed satisfactorily as a barrier in a pressurized container: Sealing Flange Thickness - 0,178 mm (.007") Outer Wall Segment Thickness - 0,178 mm (.007") adjacent the flange narrowing to 0,102 mm (.004") at the fold Inner Wall Segment Thickness - 0,102 mm (.004") adjacent the fold narrowing to 0,051 mm (.002") adjacent the central piston region Central Piston Region - 0,051 mm (.002") at the joinder of the inner wall segment and the central piston region and increasing to 0,102 mm (.004") immediately within the aforesaid joinder and thickening to 0,178 mm (.007") at the center area of the piston Length of Outer Wall Segment - 79,4 mm (3 1/8") Length of Inner Wall Segment - 65,9 mm (2 19/32") Container used with aforedescribed PET barrier was a 202 x 509 straight sided can which is 54,0 mm (2 1/8") in diameter and 141,3 mm (5 9/16") in length. The barrier had a 1° taper to each of the outer and inner wall segments, 12 and 14, respectively, to form a fold 15 providing an included angle of 2° between the outer and inner wall segments, 12 and 14. It is believed that a 3° taper to each of the inner and outer wall segments will also function satisfactorily. The central piston region for the above-described barrier had a configuration as shown in Figure 1, wherein the terminus 18 at the perimeter of the piston had a depth of 4,775 mm (0.188") and a radius of 1,60 mm (.063") The sealing flange 16 for the described barrier had a turning radius into outer wall segment 12 of 1,98 mm (.078"). Figure 2 shows the barrier 10 inserted in a valved pressure container generally designated as 22, having inner wall surface 23, and permanently joined to the container through the sealing flange 16 by an appropriate crimping of the flange 16 between the joint formed by the lower end 24 of the sidewall of the container 22 and the perimeter of the bottom closure 26 of the container 22. Without intention to limit the type of pressure container (aerosol) with which the barrier pack of this invention may be usefully employed, it has been found particularly useful when employed with an aerosol container commonly referred to as a "necked-in" container. A sealable port 28 is provided in the bottom closure 26 for introduction of propellant. A manually actuable valve (not shown) is positioned in a manner well-known to those skilled in the art in the opening 29 of the pressure container 22. In Figure 2, the barrier 10 divides the interior of the container 22 into a plural zoned pressure container; the upper zone 32 for receiving the product to be dispensed and the lower zone 34 for receiving the propellant. Generally, the container manufacturer will insert the barrier 10 into container 22, and seal the barrier to the container as described above. A product filler will thereafter fill the product and propellant into the respective chambers 32 and 34. For many applications of the barrier pack of the present invention within an aerosol container, the barrier 10, as shown in Figure 1, will be inserted and bottom sealed into the container 22 as shown in Figure 2 and as described above. Alternatively, after bottom sealing the barrier 10 within the container 22 as shown in Figure 2, and with the aerosol valve in place in the container 22, propellant may be admitted to the container 22 in the zone 34 to cause the barrier 10 to fully or partially expand (shown as fully expanded in Figure 4b) within the container 22, it being understood that the aerosol valve in the container opening, if present, must be opened to allow the barrier to expand. After the barrier 10 has expanded within the container 22, product may be pressure filled into the zone 32 to cause the barrier 10 to refold to the shape, or similar to the shape, as shown in Figure 2. A further alternative is to top seal the barrier pack of this invention, i.e. to invert the barrier pack of this invention and seal the sealing flange 16 between the top portion of the container 22 and the upper sidewall of the container 22. In such a top sealing arrangement, product may be introduced into the product zone to cause the barrier 10 to fully expand downwardly within the container 22 to substantially conform to the inner surface 23 of the container 22. During the filling of the product into the container it may be necessary to provide a means for evacuating air in the propellant zone. After introducing propellant into the propellant zone, the container is ready to function to discharge product through actuation of the aerosol valve positioned in the container opening 29. Upon complete evacuation of product from the container 22, the barrier 10 will assume a shape such as in Figure 1, wherein the inner wall 14 will be folded within the outer wall 12 but, with the sealing flange 16 being top sealed, the barrier 10 will be in an inverse relation within the container as that shown in Figure 2. In both of the alternative arrangements and procedures described immediately above, the outer wall 12 is substantially thicker and more rigid than the inner wall 14. Figure 3 shows a configuration for annexing the barrier 10 to the container 22. Figure 3 shows the barrier sealing means to be a terminal flange 16 extending from the outer wall segment 12. The flange 16 fits tightly between the flanges 24 and 26. The seam is formed by rolling the flanges 24, 26 and 16 toward the side wall 12 to form a rolled seam by techniques known to those skilled in the art. A double roll seam may be used. The thickness and length of the sealing flange 16 is dictated by the requirements of rolled seams, which may vary by type of container and rolling equipment. The sealing flange 16 may be thicker than the contiguous outer wall segment 12. The sealing flange 16 may function as a gasket in sealing the barrier to the base of the container. If necessary, an adhesive may be provided to the components that are to be roll seamed. Figure 4a shows the barrier in an initial position a short period of time after loading the container with product and propellant. During this short period of time before consumer usage, the outer wall segment 12 has expanded due to propellant pressure, from its Figure 2 position, to contact and to fully conform to the inner wall surface 23 of the container 22. Due to the frustoconical shape of the outer wall segment 12, the contact and conformance of the outer wall segment occurs progressively upwardly from flange 16 to fold 15, thereby clearing the space between the outer wall segment 12 and the inner wall surface 23 of the container 22 of product. Upon continuous or intermittent actuation of the valve disposed in the top opening of the pressurized container, product will be evacuated from the container by lowering the pressure in the product zone 32 and causing the greater pressure in the propellant zone 34 to expand the barrier against the product and force the product through the discharge valve of the container. As product is evacuated from the container 22, the inner wall segment 14 and the central piston region 20 move axially toward the aerosol discharge valve as the barrier unfolds. The barrier may be dimensioned such that after evacuation of most of the product in the container the central piston region has not yet risen high enough to shut off the product discharge orifice(s) in the valve. As evacuation nears its completion, the barrier may expand to assume the configuration shown by the dotted line in Figure 4b, it being understood that in Figure 4b the outer and inner wall segments 12 and 14 contact and fully conform to the inner wall surface 23. It has been observed that the frustoconical configuration of the inner wall segment 14, as well as the expandable nature of the barrier 10 toward the inner wall surface 23 of the container 22, results in the outer surface of the inner wall segment progressively advancing in an axial direction against the inner wall surface 23 of the pressure container to cause the progressive advance of the product to the discharge valve and a minimization of the capture or entrapment of product between the outer surface of the barrier and the inner surface of the container. Pockets are not observed to form within the barrier itself. The tapering of the outer wall segment facilitates the invagination of the barrier of the present invention into the pressurized container. The presence of the tapering of both the outer and inner wall segments, and at small angles, also allows maximum nesting of the barriers for convenience and cost savings in shipping the barriers from a manufacturing site to the site of the container manufacturing operation. At the container manufacturing site, the stacks of nested barriers facilitate fast and easy feeding of the barriers sequentially into the containers. Each nested barrier may be pulled from its stack into its intended container under the influence of an initial vacuum in the container shell, each barrier as it is inserted into its container shutting off the vacuum; alternatively each nested barrier may be blown by air from its stack into the intended container. The next container shell is fed under the stack of nested barriers, and the identical action continues for the next container and next barrier. Containers continue to be sequentially fed under the nested stacks of barriers, and the nesting provides for a high speed and very simple feeding operation. Figure 6 shows an embodiment of the central piston region 20 which includes a plurality of reinforcing ribs 100 that add to the strength of the central piston region 20. Depending on the weight and type of product being dispensed, it may be preferable to have a thicker and/or reinforced central piston region and/or thicker wall segments in order to insure uniform and complete discharge of the product. Alternatively, it may be desirable to have the central piston region thinner than the contiguous inner wall segment to enable the central piston region to expand fully into the upper recesses of the container. In order to overcome the problem of permeation of propellant and/or product through the barrier found in prior art dispensers, the flexible barrier in accordance with the present invention is optionally made of a multilayered material. Figure 5 shows a wall construction consisting of an inner layer 102 designed to prevent transport of propellant and product. Layer 102 is sandwiched between outer layers 104 and 106 that are inert to propellant or product in contact with the outer layers. Adhesive layers 108 and 110 are optionally provided, or alternatively the inner and outer layers 102, 104 and 106 may be fused together by heat or other means. In one embodiment, the inner layer 102 is a gas barrier layer and the outer layers 104 and 106 are aqueous or organic fluid barrier layers. The gas barrier layer may be made of PET, ethylene vinyl alcohol, polyvinylalcohol, polyvinylidene chloride, polyacrylonitrile, cellophane or other similarly suitable materials. The outer layers may be made of PET, polyethylene, (especially high density polyethylene) polypropylene, polytetrafluoroethylene, polybutane, surlyn ionomer, butyl rubber, polyvinylidene chloride, polychlorotrifluoroethylene, Penton, polyvinylfluoride or other similarly suitable materials. Ethylene vinyl alcohol and polyvinyl alcohol are preferred gas barrier materials and high density polyethylene is a preferred aqueous or organic fluid barrier material. Any propellants known in the art may be used with the dispenser and flexible barrier of the present invention. The barrier of the present invention requires smaller amounts of liquified propellants than required in non-barrier pack aerosol systems and in certain barrier pack systems using compressed gases, thus allowing the economic use of more expensive propellants. The present system lends itself to a maximization of the amount of product to be dispensed from a given container. The barrier pack of this invention is presently manufactured utilizing a forming process generally referred to as thermoforming. The thermoforming technique for manufacturing plastic shapes from a sheet of the plastic material is well-known in a general sense. Specific modifications of the general techniques are used to tailor the thermoforming process to the forming of a particular shape. The schematic diagram of Figure 8 shows the several steps involved in the forming of the barrier packs of this invention. In step 1, the plastic sheet material, PET, for example, having a thickness of 0,635 mm (.025"), is passed through a dry heat zone (oven) to bring the PET to a forming temperature of 121°-165°C (250°-330°F.) It is desirable to have the PET at 140°-149°C (285°-300°F.), that is, to avoid the extremes of the 121°-165°C (250°-330°F.) range. The PET material found suitable for forming the barrier packs is biaxially oriented and suitable for deep draw thermoforming. The barrier pack of this invention is a deep drawn part and thus is susceptible to "webbing", i.e. the formation of a fold of excess material at the mold base and the barrier side wall. Where "webbing" is a concern, careful control of the temperature of the plastic sheet material is critical. Moreover, with temperature control and avoidance of a temperature above the distortion temperature of the plastic sheet material, a degree of plastic memory is retained by the plastic material, this memory aiding in the preclusion or removal of the "webbing" problem. In step 2, the pre-heated PET sheet is moved to the forming station (thermoformer), whereat the PET sheet is prestretched using a "plug assist" for the initial forming of the inner wall segment and the piston region of the barrier pack and using a "ring" to partially form the outer wall segment. Also see Figure 9. The "ring" assists in the avoidance of "webbing". The "plug assist" and "ring" are mounted on the upper movable platen (top base plate) of the thermoformer equipment, directly across from the lower movable platen (base plate) on which the mold is mounted. After disposing the heated plastic sheet between the upper and lower platens, the forming operation is commenced by moving the platens toward each other to sandwich the heated sheet. During the course of moving the platens until their ultimate contacting against each other, the "plug assist" and "ring" draw the sheet into and around the interior cavity surface of the mold to force the heated PET sheet to conform and contact the mold at the fold joining the outer wall segment and the inner wall segment and at the base of the "ring". The "ring" in forcing the PET plastic sheet against the base plate of the thermoforming equipment effects an annular seal around the mold. After effecting the seal, vacuum is applied to the mold to cause the PET plastic sheet to be drawn against the mold surface and thereby complete the final shaping of the PET plastic sheet. The mold is water cooled, teflon coated aluminum, heat conductive, and the "plug assist" and "ring" are fine-grained wood covered with felt to avoid scuffing and sticking of the formed part. After adequate cooling, the upper and lower platens are separated and the formed sheet transported to the trimming station (step 3) whereat cutting dies trim the formed parts. The formed parts are ejected to a stacker and the trimmed residue at the sealing flange is ground for recycling and reclaiming in the plastic sheet extrusion process. It is believed that biaxial orientation of the plastic during the extrusion of the plastic sheet to be thermoformed and the biaxial orientation during the thermoforming process decrease the permeation of the barrier material. While the invention has been particularly shown and described with respect to illustrative and preferred embodiments thereof, it will be understood by those skilled in the art that the foregoing and other changes in form and details may be made therein without departing from the scope of the invention which is limited only by the scope of the appended claims.

Claims: A unitary flexible and expandable barrier for use in a plural-zoned, valved pressure container comprising: a shaped spatial form having a terminal sealing means (16), a flexible and expandable wall portion (11), and a central piston region (20), said sealing means, wall portion and piston region being formed as a unitary spatial form with sufficient rigidity to maintain its shape prior to insertion into and use in a plural-zoned pressure container (22); said terminal sealing means (16) being adapted for sealing in a container (22) to form a propellant zone (34) and a product zone (32); said flexible and expandable wall portion (11) having an inner wall segment (14) and an outer wall segment (12) connected by a fold (15); said central piston region (20) being connected to and extending generally inwardly from the bottom of said inner wall segment (14) to close and complete said unitary barrier member (10); said outer wall segment (12) being a steeply frustoconical shape and extending from said terminal sealing means (16) to said fold (15), said outer wall segment and fold being dimensioned for insertion into a container (22) to form an initial spaced relationship with the inner side container surface (23); said inner wall segment (14) being an oppositely-directed, steeply frustoconical shape contained within said outer wall segment (12) and extending from said fold (15); said inner wall segment (14) having sufficient flexibility to permit said inner wall segment and said central piston region (20) to move in an axially direction under the influence of propellant pressure; said outer wall segment (12) having sufficient expandability to expand outwardly under the influence of propellant pressure to progressively substantially conform to said inner side container surface (23) from said terminal sealing means (16) to said fold (15); said inner wall segment (14) having sufficient expandability to expand outwardly under the influence of propellant pressure to substantially conform to said inner side container surface (23) from said fold (15); characterized in that said, at the initial state, outer wall segment (12) being thicker and more rigid than said, at the initial state, inner wall segment (14). The barrier of claim 1, wherein said unitary barrier (10) is comprised of PET. The barrier of any of the preceding claims, wherein said unitary barrier (10) is substantially fully nestable with further identical barrier members (10), said frustoconical outer and inner wall segments (12, 14) and intervening fold (15) of each barrier nesting with the corresponding parts of said further identical barrier members. The barrier of any of the preceding claims, wherein said central piston region (20) is flexible and expandable. The barrier of any of the preceding claims, wherein said inner wall segment (14) is slightly shorter in top to bottom dimension than said outer wall segment (12). The barrier of any of the preceding claims, wherein at least a portion of said central piston region (20) is thicker and more rigid than said inner wall segment (14). The barrier of any of the preceding claims, wherein said terminal sealing means (16) is a flange extending outwardly from the bottom of the outer wall segment (12). The barrier of any of the preceding claims, wherein said central piston region (20) has an outer periphery that emerges from said inner wall segment (14) at a substantial angle to said inner wall segment. The barrier of any of the preceding claims, wherein said barrier (10) is multi-layered, the inner layer (102) being impervious to the transport of product and propellant and the outer layers (104, 106) being inert to the product or propellant contigous thereto. A dispenser comprising: a container (22) having a bottom (26), a side wall, a top, an opening (29) in said top for mounting an externally actuable valve means, and a closable opening (28) in said bottom (26) for introducing propellant into said container (22); an externally actuable valve means extending through said top opening (29) for dispensing product from within said container (22); and a unitary flexible and expandable barrier (10) of any of the preceding claims; wherein said unitary flexible and expandable barrier (10) being sealed within said container (22) so as to define a first zone (32) above said barrier (10) for holding a product in fluid communication with said valve means and a second zone (34) below said barrier (10) for holding a propellant out of fluid communication with said first zone (32). The dispenser of claim 10, wherein said terminal sealing means (16) of said barrier (10) is sealed to said container (22) between said top and said side wall of said container. The dispenser of claim 10, wherein said terminal sealing means (16) of said barrier (10) is sealed to said container (22) between said bottom (26) and said side wall of said container.

Inventors: ABPLANALP ROBERT HENRY, ABPLANALP, ROBERT HENRY
Applicants: ABPLANALP ROBERT H, ABPLANALP, ROBERT HENRY
Application year: 1994
Main classification: B67D5
IPC codes: B29C51, B29C33, B65D83, B29C35